TITLE input2_1.asc: Circular orbiting satellite
// Input for Lab2, HandsOn2_1
OPTIONS n_scrn y_comscrn n_events n_tabout n_plot y_traj n_merge y_doc 
MODULES
	environment		def,init,exec
	forces			def,exec	
	newton			def,init,exec	
END
TIMING
	traj_step 10
	int_step 0.01
	com_step 100
END
VEHICLES 1
	SATELLITE3  Sat_s1
		//Initial conditions
			lonx  0    //Vehicle longitude - deg  module newton
			latx  0    //Vehicle latitude - deg  module newton
			alt  300000    //Vehicle altitude - m  module newton
			psivgx  90    //Vehicle heading angle - deg  module newton
			thtvgx  0    //Vehicle flight path angle - deg  module newton
			dvbe  7243.2    //Vehicle speed - m/s  module newton
	END
END
ENDTIME 5800
STOP

